Open Access
表1
机翼后缘上、下缘蒙皮曲率变化规律
| 蒙皮 | 曲率变化区间/mm | 曲率变化情况 |
| 上缘 | 0~120, 280~540, 830~970 | 减小 |
| 120~280, 540~830, 970~1 299 | 增大 | |
| 下缘 | 0~110 | 减小 |
| 110~380, 380~750 | 缓慢增大 | |
| 750~1 299 | 急剧增大 |
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